发明名称 Closed loop power control for low earth orbit satellite communications system
摘要 A satellite communication system (10) includes at least one satellite communication signal repeater (12); at least one ground station (18) for transmitting a feeder link comprised of a plurality of communication signals to the at least one satellite communication signal repeater; and a plurality of user terminals (13) each receiving one of the communication signals over a user link from the at least one satellite communication signal repeater. A method includes steps of measuring a quality of at least one reference signal received by the user terminal, via the satellite; transmitting the measured quality of the reference signal received by the user terminal to the ground station; comparing the measured quality with a predetermined reference; and adjusting a transmit power of the ground station in response to a difference between the predetermined reference and measured quality. The transmit power of the ground station is adjusted so that a flux density of a downlink beam is substantially constant at the user terminal independent of the location of the user terminal in the beam. <IMAGE>
申请公布号 EP1098456(A2) 申请公布日期 2001.05.09
申请号 EP20000309656 申请日期 2000.11.01
申请人 GLOBALSTAR L.P. 发明人 WIEDEMAN, ROBERT A.;SITES, MICHAEL J.
分类号 H04B7/15;H04B7/185 主分类号 H04B7/15
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